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Active Combustion Control Valve

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX13CC22P
Agency Tracking Number: 125573
Amount: $124,962.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: A3.05
Solicitation Number: N/A
Timeline
Solicitation Year: 2012
Award Year: 2013
Award Start Date (Proposal Award Date): 2013-05-23
Award End Date (Contract End Date): 2013-11-23
Small Business Information
CA
Cameron Park, CA 95682-7230
United States
DUNS: 126253587
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Paul Phillipsen
 Principle Investigator
 (530) 672-2795
 paulp@waskengr.com
Business Contact
 Wendel Burkhardt
Title: Business Official
Phone: (530) 672-2795
Email: wendel.burkhardt@waskengr.com
Research Institution
 Stub
Abstract

Over the past decade, research into active combustion control has yielded impressive results in suppressing thermoacoustic instabilities and widening the operational range of gas-turbine combustors. Active Combustion Instability Control (ACIC) controls the combustion process such that the heat release profile is modulated to dampen the naturally occurring thermoacoustic instabilities. A major challenge to effective implementation of active combustion control is the availability of valves and actuators that provide adequate flow modulation control authority. The majority of the published work revolves around valves designed to modulate the main combustor flow. At present these valves are not designed to operate in a harsh environment and as such are required to be located outside the main flow path, reducing their control authority. To effectively meet the challenge, valves and sensors that are smaller, more responsive and robust must be developed. Ultimately the control valves are co-located with the fuel injection manifold. The trade-off for the harsh environment operation is the ability to maximize the flow modulation control authority. The objective of this research is to integrate the required control authority into an operational environment. This research initiates the development of a light weight fast-acting fuel control valve for harsh environment operation. The valve will allow the precise time dependent fuel control required for lean-burn combustor operability. In this Phase I research a proof-of-concept valve is designed, fabricated and cold-flow tested using commercially-available driver circuitry to uncover potential performance benefits and demonstrate feasibility of the approach for further development.

* Information listed above is at the time of submission. *

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